The ADFU comparison figures are far to general to draw exact figures from them:
38. From 0 - 5,000 ft and 15,000 - 20,000 ft., the Spitfire XIV is only 20 m.p.h. faster; at all other heights it is up to 60 m.p.h. faster than the Fw 190 (BMW.801D). It is estimated to have about the same maximum speed as the new Fw 190 (DB.603) at all heights.
(109G)
44. The Spitfire XIV is 40 m.p.h. faster at all heights except 16,000 ft. where it is only 10 mph faster.
And from figures like that you want to guestimate speeds of aircraft down to a few mph?
There doesnīt exist a 190A in english reports which did more than 340mph near ground afaik. So when the Spit14 did more than 355-360mph, why didnīt they mention this 190A in reports?
340 for a 190A. The AFDU report says:
38. From 0 - 5,000 ft and 15,000 - 20,000 ft., the Spitfire XIV is only 20 m.p.h. faster; at all other heights it is up to 60 m.p.h. faster than the Fw 190 (BMW.801D). It is estimated to have about the same maximum speed as the new Fw 190 (DB.603) at all heights.
Which would make the Spit XIV around 360 at sea level. The actual performance trials showed a speed of 363 at sea level, which I think fits pretty nicely with 20mph faster than a 190A.
Well, first i have to say: What is a report worth where aircrafts are compared without mentioning the exact weight, aircraft condition, power setting etc.??? NOTHING!
I agree. So why do you wish to take such a report (the AFDU comparison) and value it more highly than full performance evaluations?
Nowhere in the AFDU report does it give aircraft speeds to a greater than 5mph accuracy:
At all heights the Spitfire XIV is 30-35 mph faster in level flight
From 0 - 10,000 feet the Tempest V is 20 mph. faster than the Spitfire XIV. There is then little to choose until 22,000 feet, when the Spitfire XIV becomes 30-40 mph. faster
From 0 - 5,000 ft and 15,000 - 20,000 ft., the Spitfire XIV is only 20 m.p.h. faster; at all other heights it is up to 60 m.p.h. faster than the Fw 190
The Spitfire XIV is 40 m.p.h. faster at all heights except 16,000 ft. where it is only 10 mph faster.
They are rounding the figures to at best 5mph, possibly even 10mph.
So a 360 mph Spit XIV is easily a 363 mph (they probably didn't even do full performance trials for all aircraft at the AFDU, that was the A&AEE's job)
The "30 mph faster than a Spit IX" can easily be 27mph faster than a Spit IX, which would put the Spit IX at 336mph at sea level, coincidentally exactly the figure given by the A&AEE during their tests of the Spit IX.
We donīt know how much power the Spit had at sealevel, BUT we know it from the 2nd gear, around 1800hp, right?
The difference in climbrate is 5100-3600 = 1500ft/min.
To lift 8400lb with another 1500ft/min, you need ~450hp.
Itīs easy to see that the Spit must have had
more than 2200hp near ground.
I'll admit I don't understand this too well, and I may be very wrong, but I don't believe it had 2200hp.
I have never seen a figure of more than 2050 hp quoted for the Griffon 65, unless it's running on higher octane fuel.
I believe the actual figure was 2035hp, which is usually rounded to 2050.
I do know that the same Griffon 65 could produce 2350hp, running at 25lb boost. In the tests where it achieved 363mph at sea level, and 5110 ft/min at low level, it was running at 18lb boost. That is clearly stated in the test report.
So far we have 200-250 hp extra accounted for, which just leaves around 200 hp.
But doesn't full superchrager gear ratio take more power? Don't you have to work harder to compress the air at higher alts to maintain that 18lb boost? Would the FS gear require a lot more HP than MS geat, which is all you needed at lower alts?